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Aerodynamic Characteristics Of A Full Scale Fan In Wing Model Including Results In Ground Effect With Nose Fan Pitch Control
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Book Synopsis Aerodynamic Characteristics of a Full-scale Fan-in-wing Model Including Results in Ground Effect with Nose-fan Pitch Control by : Jerry V. Kirk
Download or read book Aerodynamic Characteristics of a Full-scale Fan-in-wing Model Including Results in Ground Effect with Nose-fan Pitch Control written by Jerry V. Kirk and published by . This book was released on 1964 with total page 154 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Note written by and published by . This book was released on 1973 with total page 446 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Subsonic Aerodynamic Characteristics of a Large-scale 1.075-pressure-ratio Tip-turbine Cruise-fan Propulsion System at Angle of Attack by : Francis J. Capone
Download or read book Subsonic Aerodynamic Characteristics of a Large-scale 1.075-pressure-ratio Tip-turbine Cruise-fan Propulsion System at Angle of Attack written by Francis J. Capone and published by . This book was released on 1969 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt: Wind tunnel tests of subsonic aerodynamic characteristics of large scale tip turbine cruise fan with 1.075 pressure ratio at angle of attack.
Book Synopsis Fan and Wing Force Data from Wind-tunnel Investgation of a 0.38-meter (15-IN.) Diameter VTOL Model Lift Fan Installed in a Two-dimensional Wing by : Joseph A. Yuska
Download or read book Fan and Wing Force Data from Wind-tunnel Investgation of a 0.38-meter (15-IN.) Diameter VTOL Model Lift Fan Installed in a Two-dimensional Wing written by Joseph A. Yuska and published by . This book was released on 1972 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt: Test data are presented for a 38-cm (15-in.) diameter, 1.28 pressure ratio model VTOL lift fan installed in a two-dimensional wing and tested in a 2.74-by 4.58-meter (9-by 15-ft)V/STOL wind tunnel. Tests were run with and without exit louvers over a wide range of crossflow velocities and wing angle of attack. Tests were also performed with annular-inlet vanes, inlet bell-mouth surface disconuities, and fences to induce fan windmilling. Data are presented on the axial force of the fan assembly and overall wing forces and moments as measured on force balances for various static and crossflow test conditions. Midspan wing surface pressure coefficient data are also given.
Book Synopsis Monthly Catalog of United States Government Publications by :
Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on with total page 1958 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Stability and Control/wind Tunnel Data Correlation by : G. R. Casteel
Download or read book Aerodynamic Stability and Control/wind Tunnel Data Correlation written by G. R. Casteel and published by . This book was released on 1971 with total page 224 pages. Available in PDF, EPUB and Kindle. Book excerpt: The general objective was to collect and analyze aerodynamic stability and control data for the XV-4B, XV-5A, and P-1127 VTOL configurations. Correlation and analysis of existing model data were made to investigate hover and transition characteristics. Particular emphasis was placed on the aerodynamic power effects, sometimes referred to as interference effects. Other areas of investigation were sometimes referred to as interference effects. Other areas of investigation were nondimensional coefficients used to present VTOL data and wind tunnel test techniques. Wind tunnel tests were conducted using an inlet only model and a jet only model to investigate special test and analysis problems for these components. The agreement between different sets of XV-4B model data was, in general, found to be poor. However, the nondimensional coefficients used by Lockheed to reduce to XV-4B model data appear to be valid parameters for this category of VTOL airplane. The jet entrainment flow was shown by experiment to be the primary cause of the XV-4B power effects, and the XV-4B jet path was experimentally and theoretically determined.
Book Synopsis Monthly Catalog of United States Government Publications by : United States. Superintendent of Documents
Download or read book Monthly Catalog of United States Government Publications written by United States. Superintendent of Documents and published by . This book was released on 1961 with total page 1248 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalog of United States Government Publications, Cumulative Index by : United States. Superintendent of Documents
Download or read book Monthly Catalog of United States Government Publications, Cumulative Index written by United States. Superintendent of Documents and published by . This book was released on 1970 with total page 1348 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :Sandra K. Faull Publisher :Arlington, Va. : United States Historical Documents Institute ISBN 13 : Total Pages :608 pages Book Rating :4.:/5 (321 download)
Book Synopsis Cumulative Title Index to United States Public Documents, 1789-1976 by : Sandra K. Faull
Download or read book Cumulative Title Index to United States Public Documents, 1789-1976 written by Sandra K. Faull and published by Arlington, Va. : United States Historical Documents Institute. This book was released on 1979 with total page 608 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development Publisher : ISBN 13 : Total Pages :344 pages Book Rating :4.X/5 (4 download)
Book Synopsis VTOL/STOL Aircraft by : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Download or read book VTOL/STOL Aircraft written by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development and published by . This book was released on 1966 with total page 344 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal Aerodynamic Characteristics of a Low-wing Lift-fan Transport Including Hover Characteristics in and Out of Ground Effect by : Danny R. Hoad
Download or read book Longitudinal Aerodynamic Characteristics of a Low-wing Lift-fan Transport Including Hover Characteristics in and Out of Ground Effect written by Danny R. Hoad and published by . This book was released on 1977 with total page 156 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Prediction methods for jet V/STOL propulsion aerodynamics by : M. F. Platzer
Download or read book Prediction methods for jet V/STOL propulsion aerodynamics written by M. F. Platzer and published by . This book was released on 1975 with total page 548 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Subsonic Performance Characteristics of a Large-scale 1.075-pressure-ratio Tip-turbine Cruise-fan Propulsion System by : Francis J. Capone
Download or read book Subsonic Performance Characteristics of a Large-scale 1.075-pressure-ratio Tip-turbine Cruise-fan Propulsion System written by Francis J. Capone and published by . This book was released on 1969 with total page 282 pages. Available in PDF, EPUB and Kindle. Book excerpt: Performance of turbine driven V/STOL cruise fan propulsion system at subsonic Mach numbers.
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1984 with total page 1278 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Survey of Lift-fan Aerodynamic Technology by :
Download or read book Survey of Lift-fan Aerodynamic Technology written by and published by . This book was released on 1993 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Large-scale Wind-tunnel Investigation of a V/STOL Transport Model with Wing-mounted Lift Fans and Fuselage-mounted Life-cruise Engines for Propulsion by : Jerry V. Kirk
Download or read book Large-scale Wind-tunnel Investigation of a V/STOL Transport Model with Wing-mounted Lift Fans and Fuselage-mounted Life-cruise Engines for Propulsion written by Jerry V. Kirk and published by . This book was released on 1967 with total page 90 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis AIAA Aerodynamic Testing Conference, Washington, D.C., March 9-10, 1964 by :
Download or read book AIAA Aerodynamic Testing Conference, Washington, D.C., March 9-10, 1964 written by and published by . This book was released on 1969 with total page 252 pages. Available in PDF, EPUB and Kindle. Book excerpt:
